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- Carbon deposition of 19 fuels in an annular turbojet combustor
- A comparison of two submerged inlets at subsonic and transonic speeds
- The effect of air-jet and strip modifications on the hydrodynamic characteristics of the streamline fuselage of a transonic airplane
- Investigation of ceramic, graphite, and chrome-plated graphite nozzles on rocket engine
- Results Obtained from Third Flight of Northrop X-4 Airplane (A.F. No. 46-676)
- Results obtained from second flight of X-4 airplane (A.F. no. 46-676)
- Effects of several leading-edge modifications on the stalling characteristics of a 45 degree swept-forward wing
- Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Aerodynamic characteristics in sideslip of a large-scale model having a 63 degree swept-back vertical tail
- Pressure-distribution measurements over an extensible leading-edge flap on two wings having leading-edge sweep of 42 degrees and 52 degrees
- Aerodynamic characteristics of a 6-percent-thick symmetrical double-wedge airfoil at transonic speeds from tests by the NACA wing-flow method
- Heat-transfer and boundary-layer transition on a heated 20 degree cone at a Mach number of 1.53
- Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 6, taper ratio 0.6, and NACA 65A009 airfoil section
- Flight Investigations at High-Subsonic, Transonic, and Supersonic Speeds to Determine Zero-Lift Drag of Fin-Stabilized Bodies of Revolution having Fineness Ratios of 12.5, 8.91, and 6.04 and Varying Positions of Maximum Diameter
- Wind-Tunnel Investigation of the Low-Speed Static Stability and Control Characteristics of a Model of Bell MX-776
- Two-Dimensional Potential Flows
- Rotationally Symmetric Potential Flows
- Wind-Tunnel Tests of a 0.16-Scale Model of the Douglas MX-656 Airplane at High Subsonic Speeds, 1, Stability and Control Characteristics
- Wind-Tunnel Tests of a 0.16-Scale Model of the Douglas MX-656 Airplane at High Subsonic Speeds. 2 - Wing and Fuselage Pressure Distribution
- Theory of Characteristics
- Rough-water Landings of a 0.1-Size Powered Dynamic Model of the XP5Y-1 Flying Boat with Two Types of Afterbody - Langley Tank Model 228 (TED No. NACA DE309)
- Effect of the Acceleration of Elongated Bodies of Revolution Upon the Resistance in a Compressible Flow
- Investigation with an interferometer of the turbulent mixing of a free supersonic jet
- Method of designing cascade blades with prescribed velocity distributions in compressible potential flows
- Altitude performance and operational characteristics of 29-inch-diameter tail-pipe burner with several fuel systems and flame holders on J35 turbojet engine
- Investigation of altitude performance of AN-F-58 fuels in annular combustor of J34-WE-22 engine
- Performance of supersonic axial-flow compressors based on one-dimensional analysis
- The effect of torsional flexibility on the rolling characteristics at supersonic speeds of tapered unswept wings
- Theoretical characteristics in supersonic flow of two types of control surfaces on triangular wings
- The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65
- Heat transfer to bodies traveling at high speed in the upper atmosphere
- Performance of Single-Stage Turbine of Mark 25 Torpedo Power Plant with Two Nozzles and Three Rotor-Blade Designs
- Development of Spoiler Controls for Remote Control of Flying Missiles
- Correlation of cylinder-head temperatures and coolant heat rejections of a multicylinder, liquid-cooled engine of 1710-cubic-inch displacement
- Use of source distributions for evaluating theoretical aerodynamics of thin finite wings at supersonic speeds
- Analysis of performance of jet engine from characteristics of components II : interaction of components as determined from engine operation
- An apparatus for varying effective dihedral in flight with application to a study of tolerable dihedral on a conventional fighter airplane
- An analysis of available data on effects of wing-fuselage-tail and wing-nacelle interference on the distribution of the air load among components of airplanes
- Performance of J33-A-21 and J33-A-23 Turbojet-Engine Compressors with Water Injection
- Performance of J33-A-27 Turbojet-Engine Compressor 1: Over-all performance characteristics at equivalent impeller speeds from 6100 to 11,800 rpm
- An NACA Vane-Type Angle-of-Attack Indicator for use at Subsonic and Supersonic Speeds
- Sound-level measurements of a light airplane modified to reduce noise reaching the ground
- Summary of section data on trailing-edge high-lift devices
- A simplified method for the determination and analysis of the neutral-lateral-oscillatory-stability boundary
- Resistance and Spray Characteristics of a 1/13-Scale Model of the Consolidated Vultee Skate 7 Seaplane: TED No. NACA DE 338
- Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane with Speedpak Attached
- Ditching Investigation of a 1/18-Scale Model of the North American B-45 Airplane
- Smooth-Water Landing Stability and Rough-Water Landing and Take-Off Behavior of a 1/13-Scale Model of the Consolidated Vultee Skate 7 Seaplane, TED No. NACA DE 338
- High-Speed Wind-Tunnel Investigation of the Lateral Stability Characteristics of a 0.10-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE 301
- Longitudinal Stability and Control Characteristics of a Semispan Wind-Tunnel Model of the XF7U-1 Airplane and a Comparison with Complete-Model Wind-Tunnel Tests and Semispan-Model Wing-Flow Tests
- Dynamics of a turbojet engine considered as a quasi-static system